A satellite reaches its intended orbit by being launched into space on a rocket. The rocket carries the satellite to a specific altitude and velocity needed to achieve orbit. Once in space, the satellite's onboard propulsion system is used to fine-tune its trajectory and adjust its speed to reach the desired orbit. The satellite must follow a precise path to ensure it stays in orbit around the Earth. **

The frequency at which a satellite orbits the Earth depends on its altitude and purpose. Most satellites in low Earth orbit (LEO) complete an orbit roughly every 90 minutes, traveling at speeds of around 28,000 kilometers per hour. Satellites in higher orbits, such as geostationary orbit, take longer to complete an orbit, typically around 24 hours. Overall, satellites orbit the Earth continuously, providing various services such as communication, weather monitoring, and navigation. **

The mass of a satellite does not play a significant role in determining its orbit. Instead, the primary factors that determine the orbit of a satellite are its velocity and the gravitational pull of the body it is orbiting. This is described by Kepler's laws of planetary motion, which state that the shape and size of an orbit are determined by the velocity and distance from the central body. Therefore, the mass of the satellite does not directly affect its orbit, as long as it is small in comparison to the body it is orbiting. **

The time it takes for a satellite to orbit the Earth depends on its altitude and speed. Low Earth orbit satellites, which are typically used for communication and Earth observation, can complete an orbit in about 90 minutes. Geostationary satellites, which orbit at a much higher altitude and are used for weather forecasting and communication, take 24 hours to complete one orbit, matching the Earth's rotation. **

An elliptical orbit is a type of orbit in which an object, such as a planet or satellite, follows an oval-shaped path around another object, typically a star or planet. In an elliptical orbit, the object's distance from the central body varies, with the closest point being the perigee and the farthest point being the apogee. The shape of the ellipse is determined by the gravitational pull of the central body and the object's velocity. Elliptical orbits are common in our solar system, with planets like Earth and Mars following elliptical paths around the Sun. **

It is not recommended to use hacks or cheats in Dark Orbit or any other online game as it violates the game's terms of service and can result in penalties such as account suspension or banning. Using hacks can also create an unfair advantage over other players, disrupting the balance of the game. It is best to play the game fairly and enjoy the experience as intended by the developers. **

The orbit of a celestial body can change due to various factors such as gravitational interactions with other objects, the presence of a third body, or the effects of general relativity. These changes can result in the orbit becoming more elliptical, shifting to a different plane, or even being ejected from its current orbit altogether. The specific changes to the orbit depend on the specific circumstances and forces at play. **

The cooling of the orbit is achieved by using a technique called drag sail deployment. This involves deploying a large, lightweight sail that increases the surface area of the satellite, allowing it to interact with the Earth's atmosphere and experience drag. The drag slows down the satellite, causing it to lose altitude and eventually re-enter the Earth's atmosphere where it will burn up upon re-entry. This controlled de-orbiting process helps to prevent the accumulation of space debris in orbit. **